참고문헌
- Yoo, D. W., Won, D. Y. and Tahk, M. J., "Optical flow based collision avoidance of multi-rotor UAVs in urban environments", International Journal of Aeronautical and Space Science, Vol.12, No. 3, 2011, pp.252-259. https://doi.org/10.5139/IJASS.2011.12.3.252
- Mueller, T. J., "Aerodynamic measurements at low Reynolds numbers for fixed wing micro-air vehicles", RTO AVT/VKI Special Course on Development and Operation of UAVs for Military and Civil Applications, 1999.
- Najafi, Y., Design of a High Altitude Long Endurance Solar Powered UAV, M.S. Thesis, San Jose State University, 2011.
- Santhanakrishnan, A., Pern, N. J., Ramakumar, K., Simpson, A. and Jacob, J. D., "Enabling flow control technology for low speed UAVs", AIAA Infotech(c)Aerospace, Arlington, Virginia, USA, 2005, AIAA 2005-6960.
- Selig, M. S., "Low Reynolds Number Airfoil Design", VKI Lecture Series - Low Reynolds Number Aerodynamics on Aircraft Including Applications in Emerging UAV Technology, 2003, RTO/AVT-VKI-104.
- Pelletier, A. and Mueller, T. J., "Low Reynolds number aerodynamics of low-aspect-ratio, thin/flat/cambered-plate wings", Journal of Aircraft, Vol. 37, No. 5, 2000, pp.825-832. https://doi.org/10.2514/2.2676
- Sohn, M. H. and Chung, H. S., "Control of delta-wing vortex by apex strake", KSAS International Journal, Vol. 8, No. 2, 2007, pp.98-106.
- Blackwelder, R. F. and Gad-el-Hak M., "Method and apparatus for reducing turbulent skin friction", US Patent US 4932612 A, 1990.
- Godard, G. and Stanislas, M., "Control of a decelerating boundary layer Part 1: Optimization of passive vortex generators", Aerospace Science and Technology, Vol. 10, 2006, pp.181-191. https://doi.org/10.1016/j.ast.2005.11.007
- Ruffin, S. M., Gupta, A. and Marshall, D., "Supersonic Channel Airfoils for Reduced Drag", AIAA Journal, Vol. 38, No. 3, 2000, pp.480-486. https://doi.org/10.2514/2.985
- Saric, W. S. and Reed, H. L., "Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness", 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA, 2002, AIAA 2002-0147.
- Oruc, V., "Passive control of flow structures around a circular cylinder by using screen", Journal of Fluids and Structures, Vol. 33, 2012, pp.229-242. https://doi.org/10.1016/j.jfluidstructs.2012.05.002
- Kral, L. D., "Active flow control technology", ASME Fluids Engineering Division Technical Brief, 2000.
- Jahanmiri M.. "Active flow control: A review", Research report, 2010, ISSN 1652-8549.
- Lee, K. Y., Chung, H. S. and Cho, D. H., "A PIV Study of Flow Patterns Over Stationary and Pitch-Oscillating Airfoils with Blowing Jet", KSAS International Journal, Vol. 9, No. 1, 2008, pp. 111-120.
- Sinha, S. K. and Ravande, S. V., "Drag Reduction of Natural Laminar Flow Airfoil with a Flexible Surface Deturbulator", 3rd AIAA Flow Control Conference, San Francisco, CA, USA, 2006, AIAA 2006-3030.
- Cho, Y. C. and Shyy, W., "Adaptive flow control of low-Reynolds number aerodynamics using dielectric barrier discharge actuator", Progress in Aerospace Sciences, Vol. 47, 2011, pp.495-521. https://doi.org/10.1016/j.paerosci.2011.06.005
- Moreau, E., "Airflow control by non-thermal plasma actuators", Journal of Physics D: Applied Physics, Vol. 40, No. 3, 2007, pp. 605-636. https://doi.org/10.1088/0022-3727/40/3/S01
- Benard, N., Jolibois. J., Mizuno, A. and Moreau, E., "Innovative Three-Electrode Design for Definition of Multiple Dielectric Barrier Discharge Actuators", ESA/IEEEIAS/ IEJ/SFE Joint Conference on Electrostatic, Boson, USA, 2009.
- Huang, J., Corke, T. C. and Thomas, F. O., "Plasma Actuators for Separation Control of Low-Pressure Turbine Blades", AIAA Journal, Vol. 44, No. 1, 2006, pp. 51-57. https://doi.org/10.2514/1.2903
- Jukes, T., Segawa, T. and Walker, S., "Active Separation Control over a NACA0024 by DBD Plasma Actuator and FBG Sensor", Journal of Fluid Science and Technology, Vol. 7, No. 1, 2012, pp. 39-52. https://doi.org/10.1299/jfst.7.39
- Vorobiev, A., Rennie, R. M. and Jumper, E. J., "Lift Enhancement by Plasma Actuators at Low Reynolds Numbers", 5th AIAA Flow Control Conference, AIAA 2010-483.
- Rethmel, C., Little, J., Takashima, K. Sinha, A., Adamovich, I. and Samimy, M., "Flow Separation Control over an Airfoil with Nanosecond Pulse Driven DBD Plasma Actuators", AIAA Journal, AIAA 2011-487.
- Menghu, Han, Jun, L., Zhongguo, N., Hua, L., Huangyin, Z. and Weizhuo, H., "Aerodynamic performance enhancement of a flying wing using nanosecond pulsed DBD plasma actuator", Chinese Journal of Aeronautics, Vol. 28, 2015.
- Tabatabaeian, S., Mirzaei, M., Sadighzadeh, A., Damideh, V. and Shadaram, A., "Experimental investigation of the effects of various plasma actuator configuration on lift and drag coefficients of a circular cylinder including the effects of electrodes", Chinese Journal of Aeronautics, Vol. 25, 2012, pp.311-324. https://doi.org/10.1016/S1000-9361(11)60392-0
- Klimov, A., Moralev, I., Bityurin, V.A., Kazansky, P.N., Chertov, D.A. and Borisov I.A, "Flow Around Wing Model with a Surface HF Discharge", 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, USA, 2001, AIAA 2011-1146.
- Porter, C. O., Baughn, J. W., McLaughlin, T. E., Enloe, C. L. and Font, G. I., "Temporal Force Measurements on an Aerodynamic Plasma Actuator", 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2006-104.
- Moreau, E., Sosa, R., and Artana, G., "Electric wind produced by surface plasma actuators: a new dielectric barrier discharge based on a three-electrode geometry", Journal of Physics D: Applied Physics, Vol. 41, No. 11, 2008, 115204 (12 pp). https://doi.org/10.1088/0022-3727/41/11/115204
- Ye, Q., Wu, Y., Li, X., Chen, T. and Shao, G., "Uniformity of dielectric barrier discharges using mesh electrodes", Plasma Sources Science and Technology, Vol. 21, No. 6, 2012, 065008 (7 pp). https://doi.org/10.1088/0963-0252/21/6/065008
- Grange, F., Soulem, N., Loiseau. J. F. and Spyrou, N., "Numerical and experimental determination of ionizing front velocity in a DC point-to-plane corona discharge," Journal of Physics D: Applied Physics, Vol. 28, No. 8, 1995, pp. 1619-1629. https://doi.org/10.1088/0022-3727/28/8/011
- Shin, J. and Raja, L. L., "Cathode-sheath driven lowspeed aerodynamic flow actuation using direct-current surface glow discharges", Journal of Electrostatics, Vol. 68, No. 5, 2010, pp. 453-457. https://doi.org/10.1016/j.elstat.2010.06.010
- Sosa, R. and Artana, G., "Steady control of laminar separation over airfoils with plasma sheet actuators", Journal of Electrostatics, Vol. 68, No. 7-9, 2006, pp. 604-610.
- Roth, J. R., "Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a one atmosphere uniform glow discharge plasma", Physics of Plasmas, Vol. 10, No. 5, 2003, pp. 2116-2126.
- Stark, R. H. and Schoenbach, K. H., "Direct current high-pressure glow discharges", Journal of Applied Physics, Vol. 85, No. 4, 1999, pp. 2075-2080. https://doi.org/10.1063/1.369505
- Raizer, Yu. P., Gas Discharge Physics, Springer, New York, 1991.
- Roupassov, D. V., Nikipelov, A. A., Nudnova, M. M. and Starikovskii, A. Yu., "Flow separation control by plasma actuator with nanosecond pulsed-periodic discharge," AIAA Journal, Vol. 47, No. 1, 2009, pp. 168-185. https://doi.org/10.2514/1.38113